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EPPLER 1210 AIRFOIL (e1210-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: EPPLER 1210 AIRFOIL (e1210-il)
Reynolds number: 1,000,000
Max Cl/Cd: 117.13 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e1210-il-1000000-n5.txt
Download as CSV file: xf-e1210-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: EPPLER 1210 AIRFOIL                             
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -0.6213   0.10213   0.09953  -0.0423   1.0000   0.0143
 -15.250  -0.6334   0.09648   0.09384  -0.0455   1.0000   0.0145
 -14.750  -1.0530   0.03019   0.02641  -0.0955   1.0000   0.0129
 -14.500  -1.0558   0.02793   0.02402  -0.0944   1.0000   0.0130
 -14.250  -1.0319   0.02607   0.02204  -0.0968   0.9976   0.0131
 -14.000  -1.0059   0.02426   0.02012  -0.0992   0.9936   0.0134
 -13.750  -0.9832   0.02282   0.01859  -0.1002   0.9880   0.0137
 -13.500  -0.9582   0.02164   0.01733  -0.1010   0.9800   0.0139
 -13.250  -0.9361   0.02064   0.01626  -0.1009   0.9615   0.0142
 -13.000  -0.8745   0.01934   0.01486  -0.1086   0.9347   0.0148
 -12.750  -0.8345   0.01860   0.01382  -0.1116   0.8670   0.0153
 -12.500  -0.8152   0.01816   0.01316  -0.1102   0.8236   0.0156
 -12.250  -0.7949   0.01762   0.01247  -0.1091   0.7944   0.0161
 -12.000  -0.7736   0.01707   0.01179  -0.1082   0.7705   0.0166
 -11.750  -0.7512   0.01657   0.01117  -0.1073   0.7492   0.0172
 -11.500  -0.7278   0.01613   0.01062  -0.1066   0.7311   0.0178
 -11.250  -0.7038   0.01573   0.01011  -0.1059   0.7139   0.0184
 -11.000  -0.6798   0.01528   0.00956  -0.1052   0.6978   0.0192
 -10.750  -0.6550   0.01486   0.00907  -0.1046   0.6832   0.0202
 -10.500  -0.6297   0.01451   0.00863  -0.1040   0.6693   0.0211
 -10.250  -0.6044   0.01414   0.00818  -0.1035   0.6556   0.0222
 -10.000  -0.5786   0.01379   0.00776  -0.1030   0.6428   0.0235
  -9.750  -0.5524   0.01349   0.00740  -0.1025   0.6310   0.0248
  -9.500  -0.5263   0.01317   0.00701  -0.1020   0.6184   0.0263
  -9.250  -0.4996   0.01289   0.00667  -0.1015   0.6079   0.0278
  -8.750  -0.4461   0.01236   0.00603  -0.1007   0.5855   0.0311
  -8.500  -0.4192   0.01213   0.00574  -0.1003   0.5745   0.0329
  -8.250  -0.3918   0.01190   0.00547  -0.0999   0.5647   0.0350
  -8.000  -0.3647   0.01170   0.00521  -0.0995   0.5543   0.0370
  -7.750  -0.3370   0.01150   0.00498  -0.0992   0.5453   0.0392
  -7.250  -0.2817   0.01114   0.00454  -0.0985   0.5266   0.0432
  -7.000  -0.2540   0.01100   0.00434  -0.0981   0.5175   0.0451
  -6.750  -0.2260   0.01084   0.00415  -0.0978   0.5097   0.0474
  -6.500  -0.1980   0.01072   0.00398  -0.0975   0.5001   0.0495
  -6.250  -0.1701   0.01057   0.00381  -0.0972   0.4925   0.0521
  -6.000  -0.1418   0.01046   0.00366  -0.0969   0.4847   0.0545
  -5.750  -0.1140   0.01035   0.00352  -0.0966   0.4761   0.0577
  -5.500  -0.0856   0.01024   0.00339  -0.0963   0.4686   0.0607
  -5.250  -0.0575   0.01015   0.00326  -0.0961   0.4606   0.0639
  -4.750  -0.0007   0.00998   0.00304  -0.0955   0.4474   0.0690
  -4.500   0.0275   0.00993   0.00295  -0.0953   0.4393   0.0717
  -4.250   0.0560   0.00986   0.00285  -0.0950   0.4330   0.0741
  -4.000   0.0844   0.00979   0.00277  -0.0948   0.4262   0.0770
  -3.500   0.1413   0.00970   0.00263  -0.0943   0.4144   0.0825
  -3.250   0.1698   0.00966   0.00257  -0.0941   0.4074   0.0854
  -3.000   0.1981   0.00966   0.00252  -0.0938   0.4005   0.0880
  -2.750   0.2267   0.00961   0.00246  -0.0936   0.3952   0.0911
  -2.500   0.2551   0.00958   0.00242  -0.0934   0.3894   0.0944
  -2.000   0.3120   0.00956   0.00235  -0.0929   0.3781   0.1005
  -1.750   0.3404   0.00955   0.00233  -0.0927   0.3718   0.1039
  -1.500   0.3686   0.00959   0.00232  -0.0925   0.3657   0.1068
  -1.250   0.3971   0.00956   0.00230  -0.0923   0.3614   0.1109
  -1.000   0.4255   0.00956   0.00229  -0.0921   0.3560   0.1148
  -0.750   0.4537   0.00961   0.00230  -0.0918   0.3500   0.1180
  -0.500   0.4820   0.00961   0.00230  -0.0916   0.3450   0.1226
  -0.250   0.5104   0.00962   0.00231  -0.0914   0.3406   0.1275
   0.000   0.5386   0.00966   0.00233  -0.0912   0.3354   0.1315
   0.250   0.5664   0.00970   0.00236  -0.0910   0.3297   0.1372
   0.500   0.5948   0.00972   0.00238  -0.0908   0.3259   0.1429
   0.750   0.6229   0.00974   0.00241  -0.0906   0.3216   0.1500
   1.000   0.6509   0.00979   0.00246  -0.0904   0.3172   0.1575
   1.250   0.6786   0.00984   0.00251  -0.0901   0.3125   0.1677
   1.500   0.7068   0.00987   0.00256  -0.0899   0.3091   0.1782
   1.750   0.7347   0.00990   0.00262  -0.0897   0.3047   0.1929
   2.000   0.7623   0.00994   0.00269  -0.0895   0.3006   0.2111
   2.250   0.7897   0.00999   0.00277  -0.0892   0.2965   0.2328
   2.500   0.8175   0.00999   0.00285  -0.0891   0.2939   0.2637
   2.750   0.8452   0.00999   0.00294  -0.0889   0.2907   0.2982
   3.000   0.8725   0.01000   0.00304  -0.0886   0.2867   0.3403
   3.250   0.8994   0.01002   0.00316  -0.0884   0.2824   0.3953
   3.500   0.9264   0.01001   0.00328  -0.0881   0.2792   0.4555
   3.750   0.9535   0.00996   0.00341  -0.0879   0.2768   0.5304
   4.000   0.9801   0.00988   0.00354  -0.0876   0.2739   0.6187
   4.250   1.0058   0.00981   0.00370  -0.0871   0.2707   0.7162
   4.500   1.0280   0.00965   0.00387  -0.0857   0.2674   0.8476
   4.750   1.0611   0.00961   0.00401  -0.0865   0.2636   1.0000
   5.000   1.0881   0.00974   0.00413  -0.0862   0.2611   1.0000
   5.250   1.1148   0.00988   0.00426  -0.0859   0.2584   1.0000
   5.500   1.1412   0.01005   0.00440  -0.0855   0.2554   1.0000
   5.750   1.1672   0.01023   0.00455  -0.0851   0.2524   1.0000
   6.000   1.1930   0.01043   0.00472  -0.0847   0.2492   1.0000
   6.250   1.2193   0.01058   0.00487  -0.0843   0.2472   1.0000
   6.500   1.2454   0.01074   0.00502  -0.0839   0.2446   1.0000
   6.750   1.2711   0.01092   0.00519  -0.0835   0.2416   1.0000
   7.000   1.2963   0.01112   0.00537  -0.0830   0.2386   1.0000
   7.250   1.3211   0.01135   0.00557  -0.0824   0.2356   1.0000
   7.500   1.3461   0.01155   0.00577  -0.0819   0.2333   1.0000
   7.750   1.3713   0.01173   0.00596  -0.0814   0.2314   1.0000
   8.000   1.3962   0.01192   0.00615  -0.0809   0.2292   1.0000
   8.250   1.4204   0.01213   0.00636  -0.0803   0.2265   1.0000
   8.500   1.4439   0.01238   0.00660  -0.0796   0.2236   1.0000
   8.750   1.4666   0.01266   0.00686  -0.0787   0.2205   1.0000
   9.000   1.4900   0.01288   0.00709  -0.0780   0.2185   1.0000
   9.250   1.5133   0.01310   0.00732  -0.0773   0.2168   1.0000
   9.500   1.5360   0.01333   0.00757  -0.0764   0.2148   1.0000
   9.750   1.5577   0.01359   0.00784  -0.0755   0.2125   1.0000
  10.000   1.5781   0.01387   0.00812  -0.0743   0.2100   1.0000
  10.250   1.5959   0.01419   0.00844  -0.0727   0.2073   1.0000
  10.500   1.6131   0.01450   0.00876  -0.0710   0.2051   1.0000
  10.750   1.6316   0.01477   0.00906  -0.0695   0.2037   1.0000
  11.000   1.6494   0.01507   0.00938  -0.0679   0.2018   1.0000
  11.250   1.6663   0.01541   0.00975  -0.0663   0.1996   1.0000
  11.500   1.6821   0.01580   0.01015  -0.0646   0.1974   1.0000
  11.750   1.6967   0.01625   0.01062  -0.0628   0.1950   1.0000
  12.000   1.7094   0.01680   0.01117  -0.0608   0.1922   1.0000
  12.250   1.7253   0.01723   0.01164  -0.0594   0.1908   1.0000
  12.500   1.7400   0.01772   0.01217  -0.0578   0.1887   1.0000
  12.750   1.7532   0.01831   0.01280  -0.0562   0.1863   1.0000
  13.000   1.7644   0.01904   0.01354  -0.0545   0.1838   1.0000
  13.250   1.7741   0.01989   0.01442  -0.0528   0.1813   1.0000
  13.500   1.7830   0.02085   0.01540  -0.0511   0.1791   1.0000
  13.750   1.7955   0.02166   0.01627  -0.0500   0.1775   1.0000
  14.000   1.8065   0.02260   0.01726  -0.0488   0.1759   1.0000
  14.250   1.8162   0.02368   0.01839  -0.0476   0.1737   1.0000
  14.500   1.8239   0.02496   0.01970  -0.0465   0.1715   1.0000
  14.750   1.8297   0.02644   0.02123  -0.0454   0.1693   1.0000
  15.000   1.8336   0.02815   0.02297  -0.0444   0.1671   1.0000
  15.250   1.8414   0.02961   0.02449  -0.0437   0.1654   1.0000
  15.500   1.8481   0.03121   0.02615  -0.0430   0.1635   1.0000
  15.750   1.8528   0.03303   0.02802  -0.0424   0.1614   1.0000
  16.000   1.8542   0.03519   0.03024  -0.0419   0.1589   1.0000
  16.250   1.8524   0.03771   0.03281  -0.0414   0.1565   1.0000
  16.500   1.8510   0.04028   0.03543  -0.0410   0.1540   1.0000
  16.750   1.8527   0.04258   0.03780  -0.0408   0.1521   1.0000
  17.000   1.8509   0.04531   0.04059  -0.0407   0.1493   1.0000
  17.250   1.8440   0.04868   0.04401  -0.0407   0.1462   1.0000
  17.500   1.8349   0.05239   0.04777  -0.0410   0.1437   1.0000
  17.750   1.8327   0.05540   0.05086  -0.0412   0.1417   1.0000
  18.000   1.8274   0.05885   0.05438  -0.0417   0.1391   1.0000
  18.250   1.8176   0.06291   0.05850  -0.0424   0.1361   1.0000
  18.500   1.8037   0.06761   0.06326  -0.0433   0.1333   1.0000
  18.750   1.7946   0.07179   0.06752  -0.0443   0.1307   1.0000
  19.000   1.7860   0.07598   0.07177  -0.0453   0.1277   1.0000
  19.250   1.7714   0.08106   0.07691  -0.0467   0.1244   1.0000
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